EP3540211A1 - Vortex generator for attachment to a wind energy assembly rotor blade - Google Patents
Vortex generator for attachment to a wind energy assembly rotor blade Download PDFInfo
- Publication number
- EP3540211A1 EP3540211A1 EP18161546.9A EP18161546A EP3540211A1 EP 3540211 A1 EP3540211 A1 EP 3540211A1 EP 18161546 A EP18161546 A EP 18161546A EP 3540211 A1 EP3540211 A1 EP 3540211A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- vortex generator
- base
- rotor blade
- fins
- length
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
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Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape of the blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape of the blades
- F03D1/0641—Rotors characterised by their aerodynamic shape of the blades of the section profile of the blades, i.e. aerofoil profile
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/065—Rotors characterised by their construction elements
- F03D1/0675—Rotors characterised by their construction elements of the blades
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/667—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/60—Assembly methods
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/10—Stators
- F05B2240/12—Fluid guiding means, e.g. vanes
- F05B2240/122—Vortex generators, turbulators, or the like, for mixing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/21—Rotors for wind turbines
- F05B2240/221—Rotors for wind turbines with horizontal axis
- F05B2240/2212—Rotors for wind turbines with horizontal axis perpendicular to wind direction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/301—Cross-section characteristics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/306—Surface measures
- F05B2240/3062—Vortex generators
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Definitions
- Vortex generators are used in wind turbine rotor blades for a specific influencing of the flow conditions. They have two fins arranged at a distance from each other, each projecting from the surface of the rotor blade into a boundary layer of the flow and which are aligned at an angle to the direction of flow. If these fins are exposed to the incoming air in the operation of the rotor blade, this leads to the formation of high-energy vortices and downstream of the vortex generator to a turbulent boundary layer. In particular, in the leaf root area, it has been found useful in many cases to use this effect to avoid or delay flow separation. For this purpose, the vortex generators must be attached to appropriate positions on the leaf surface. This is usually done by sticking.
- This attachment encounters considerable difficulties. Basically, there are high demands on the quality of the attachment, because during operation, the rotor blades of wind turbines are exposed to wind and weather for years and difficult to access for maintenance and repair work.
- the surface of the rotor blades has a curvature that changes continuously both in the direction of the blade depth, ie from the profile nose edge to the profile end edge, and in the longitudinal direction of the rotor blade, ie from the blade root to the blade tip.
- Vortex generators have become known which have a curved mounting surface for adhering to the surface of a wind turbine rotor blade.
- the attachment surface comprises a large-area recess in which the adhesive is to be arranged, and a peripheral edge which is intended to protect the adhesive layer from external influences.
- Vortex generators have become known, which are attached with adhesive tapes to a surface of a wind turbine rotor blade.
- the vortex generators should be flexible, so that a mounting surface of the vortex generators can adapt to the contour of the rotor blade.
- Vortex generators have become known with two fins, which are interconnected by a base plate.
- the fins have a slight curvature, which should increase flexibility of the base plate and allow adaptation of the base plate to different curvatures of the surface of the rotor blade.
- Base plate U-, V-, or W-shaped form This measure is intended to allow thermal expansion and at the same time be aerodynamically advantageous.
- the vortex generator has a longitudinal direction, two fins each arranged at an angle to the longitudinal direction and extending in the longitudinal direction over a first length, and a base connecting the two fins with each other, wherein the base has a width and extending in the longitudinal direction over a second length, wherein over the entire width of the base, the second length is smaller than the first length.
- the longitudinal direction corresponds to a Auslegungsanströmraum, ie the direction in which the vortex generator is flowed in the regular operation of the incoming air. If the vortex generator is attached to the surface of a wind turbine rotor blade, the longitudinal direction lies in a profile plane of the rotor blade.
- the direction pointing to a profile nose edge of the rotor blade is called forward, the direction pointing to a profile end edge is referred to as the rear.
- the indication below refers to the direction toward the surface of the rotor blade and the indication above refers to the direction away from that surface.
- the fins extend upwardly from the base, in particular approximately orthogonally to the surface of the wind turbine rotor blade. However, you can also deviating more or less inclined to the surface arranged be.
- the fins have a height that can be adapted to the thickness of a boundary layer of the flow. In particular, the height may be slightly larger than the thickness of the boundary layer.
- the fins may have a uniform height over their entire length. Alternatively, the height may vary over the lengthwise direction.
- vortex generators whose height is less at a front end than a rear end are common. In this case, the fins may be substantially trapezoidal or triangular. Deviations are possible, both with curved front, rear, upper and / or lower edges, as well as with more or less rounded corners.
- a surface in which the respective fin is arranged may be flat or slightly curved. Both fins are arranged at an angle to the longitudinal direction. This angle may be, for example, in the range of 5 ° to 45 °, so that the two fins are oriented relative to each other at an angle in the range of 10 ° to 90 °.
- the two fins can in particular be arranged mirror-symmetrically to a longitudinal axis of the vortex generator aligned in the longitudinal direction.
- a special feature of the invention is that over the entire width of the base, the second length is smaller than the first length, that in other words the base does not extend in the flow direction over the entire length of the fins.
- the extension of the base in the longitudinal direction is meant the entire extent of the base in this direction, that is, from a forwardmost point of the base to a rearmost point of the base.
- the base may be strip-shaped with parallel front and rear edges. In this case, the distance between the leading edge and the trailing edge of the base corresponds to the second length.
- the base Transverse to the longitudinal direction, the base has a width extending from one fin to the other fin. Because of the angular position of the fins For example, the base may be trapezoidal in particular when the viewing direction is directed towards the surface. Alternatively, the base can also survive laterally over the fins.
- Typical dimensions of the entire vortex generator are, for example, in a range between a length of 2 cm and a width of 1.5 cm to a length of 25 cm and a width of 20 cm, the height of the fins, for example, in a range between 20% and 100% of the length can be.
- the base or the entire vortex generator may consist of a relatively stiff, inflexible material such as metal.
- a fiber composite material is an alternative.
- the vortex generator can be made in one piece or composed of several elements.
- the invention makes use of the fact that in the case of wind turbine rotor blades the position-dependent change of the curvature of the surface in the longitudinal direction is particularly pronounced.
- the intended shortening of the length of the base in this longitudinal direction reduces the gaps which occur between the fastening surface and the surface of the rotor blade.
- the inventors have recognized that the gap dimensions that occur can be reduced to a sufficiently short base so that they can be compensated, for example, by the elasticity of a double-sided adhesive tape. For example, 1.5 mm thick tapes can be used, which due to their elasticity, can compensate for up to about 25% of their thickness. If the base is shortened so much that the size of the gaps occurring at the different attachment positions does not change by more than about 0.375 mm, then a reliable and particularly simple attachment with such an adhesive tape is possible. However, advantages also arise when using other adhesives.
- the second length is at most 70% of the first length.
- the second length may also be at most 50%, at most 40%, at most 30% or not more than 20% of the first length.
- the base has a mounting surface for bonding to a surface of a wind turbine rotor blade.
- the attachment surface is located at an underside of the base.
- the attachment surface may optionally extend over the entire underside of the base or over a portion thereof, in particular over much of the total area of the underside of the base.
- the mounting surface may have an activated surface to ensure a particularly secure connection with the adhesive.
- the attachment surface has a curvature in the longitudinal direction.
- the mounting surface can also be flat.
- a particularly concave curvature allows a further reduction in the gap dimensions that occur, in particular if it is adapted to a mean curvature of the surface of the wind turbine rotor blade.
- the fins each have a central longitudinal portion, the lower edge of which is connected to the base, and a front longitudinal portion, which is arranged in front of the base in the longitudinal direction, and a rear longitudinal portion, which is arranged in the longitudinal direction behind the base ,
- the front longitudinal portion and the rear longitudinal portion are not connected directly to the base.
- the base is in a middle position and the fins are sufficiently fixed over their entire length.
- An attachment of the front longitudinal section or the rear longitudinal section on the surface of the rotor blade is not required in the invention and also not provided. Regardless of this, a sealing of the free space between the longitudinal sections mentioned and the surface of the rotor blade can be useful.
- the front longitudinal portion is arranged in a plane and has a lower edge projecting down over the base and / or the rear longitudinal portion is arranged in a plane and has a lower edge which projects down over the base ,
- the distance between the lower edges of the fins and the surface of the rotor blade can be reduced in this way, which can be aerodynamically advantageous.
- the lower edge of the front longitudinal section and / or the lower edge of the rear longitudinal section is curved.
- these edges may be adapted to a mean curvature or to a minimum curvature of the surface of the wind turbine rotor blade.
- the curvature can contribute to a small distance between the fin and the surface.
- a front longitudinal section and / or a rear longitudinal section of a fin has an angled edge section at its lower edge.
- the edge portion may protrude from a plane in which the longitudinal portion is arranged. In particular, it may extend from the edge to the outside, that is, away from the other fin, or to the inside, than toward the other fin.
- the angled edge section causes a stiffening of the fin and can counteract vibrations.
- the vortex generator is manufactured by punching out a flat material and then bending the two fins relative to the base. This type of production is particularly easy. By bending a high dimensional stability is achieved.
- the flat material may in particular be a sheet, for example made of aluminum or steel, in particular stainless steel.
- the flat material may have a uniform thickness, for example in the range of 0.3 mm to 3 mm.
- the aforementioned edge portions at the lower edges of front and / or rear longitudinal portions of the fins can also be formed by simple angling.
- a double-sided adhesive tape is adhered to the mounting surface.
- the adhesive tape may have an elastic layer, in particular made of foam and / or with a thickness of, for example, 1 mm or more. This allows the already explained compensation of different gaps.
- the vortex generator can be particularly easily glued to the surface of a wind turbine rotor blade without further preparation.
- the double-sided adhesive tape extends over the entire width of the attachment surface or the base and / or over the entire second length. This allows a full-surface bonding.
- a vortex generator according to any one of claims 1 to 11 is combined with a wind turbine rotor blade, wherein the mounting surface of the vortex generator is bonded to a surface of the wind turbine rotor blade.
- the bond can be made in particular with a double-sided adhesive tape.
- a seal is disposed between the surface and edges of the vortex generator adjacent the surface.
- the seal can be performed, for example, with a sealant, such as a silicone material. It may orbit around the attachment surface and / or be disposed between lower edges of the fins and the surface.
- the seal protects the bond from external influences.
- accumulation of soiling can be prevented.
- the seal leads to an optimal aerodynamic shape.
- a plurality of identically shaped vortex generators are bonded to the surface at different positions on the surface where the surface has different curvatures.
- An individual adaptation of the geometry of the vortex generators to differently curved surfaces is not necessary in the invention.
- FIG. 1 1 shows an exemplary wind turbine rotor blade 100 having a rotor blade root portion 106 with a substantially circular cross-section, a transition region 107 and a profile region 108.
- the wind turbine rotor blade 100 has a pressure side 109 and an opposite suction side 110 with respect to a longitudinal extension direction 111.
- the rotor blade 100 is formed substantially hollow inside.
- On a surface 14 of the suction side 110, the rotor blade 100 has a number of vortex generators 10.
- the vortex generator 10 off Fig. 2 is attached to a surface 14 of a wind turbine rotor blade 100, shown in partial section along a profile plane. It has two fins 16 and a base 18. The fins 16 each extend in the longitudinal direction 12 over a first length L1. The base 18 has a width B and extends in the longitudinal direction 12 over a second length L2, which is smaller than the first length L1.
- the base 18 is strip-shaped, with the width B of the strip extending transversely to the longitudinal direction 12.
- the base 18 is a total of trapezoidal.
- the base 18 is connected to central longitudinal sections 20 of the fins 16.
- the base 18 On its underside, it has one of the surface 14 facing, also flat mounting surface. Between the mounting surface and the surface 14, a double-sided adhesive tape 34 is arranged.
- the fins 16 have a height H which is greater at their rear end than at their front end.
- a front longitudinal section 22 is arranged, which is not directly connected to the base 18.
- a rear longitudinal section 24 is arranged, which is likewise not directly connected to the base 18.
- the three longitudinal sections 20, 22, 24 of the fins 16 are each arranged in a plane which is oriented perpendicular to the base or surface 14 of the wind turbine rotor blade and at an angle ⁇ to the longitudinal direction 12th
- the vortex generator 10 is mirror-symmetrical to a longitudinal axis 26. This applies in particular to the arrangement of the two fins 16.
- the front longitudinal section 22 has a lower edge 28.
- the central longitudinal section 20 has a lower edge 30, at which the fin 16 merges into the base 18.
- the rear longitudinal section 24 has a lower edge 32.
- the lower edges 28, 30, 32 are in the embodiment of Fig. 2 lined up in a straight line.
- the vortex generator 10 off Fig. 3 largely corresponds to that of Fig. 2 , The only difference is that the front longitudinal sections 22 and the rear longitudinal sections 24 of the fins 16 each have an edge section 36 which extends inwardly from the respective lower edge 28 or 32 of the respective longitudinal section 22, 24. These edge portions 36 are arranged in the same plane as the base 18th
- the vortex generator 10 off Fig. 4 also largely corresponds to that Fig. 2 , The only difference is that the lower edges 28 and 32 of the front longitudinal sections 22 and the rear longitudinal sections 24 of the fins 16 are curved. They run at approximately uniform distance from the surface 14. These lower edges 28, 32 are down over the base 18 via.
- the vortex generator 10 off Fig. 5 largely corresponds to that of Fig. 3 , The only difference is that the lower edges 28, 32 of the front longitudinal section 22 and the rear longitudinal section 24 of the fins 16, similar to the vortex generator 10 from Fig. 4 survive down over the base 18. In contrast to the vortex generator 10 off Fig. 4 However, they run straight.
- the vortex generator 10 off Fig. 6 largely corresponds to that of Fig. 4 , The only difference is that not only the lower edges 28, 32 of the front longitudinal section 22 and the rear longitudinal section 24 of the fins 16 are curved, but also that the base 18 has a curvature. This curvature of the base 18 corresponds to a mean curvature of the surface 14 of the wind turbine rotor blade. In addition, a seal 38 is shown, which fills a space between the edges of the vortex generator 10 and the surface 14.
- Fig. 7 shows a stamped part 40 made of sheet steel, which has a base 18 and two fins 16.
- Middle longitudinal sections 20 of the fins 16 go to the dashed lines, the course of which corresponds to the lower edges 30 of the central longitudinal sections 20, in the base 18 via. It is intended to angle the fins 16 along the dashed lines relative to the base 18.
- the lower edges 28 and 32 of the front longitudinal sections 22 and rear longitudinal sections 24 of the fins 16 are curved, so that by this raising of the fins 16, a vortex generator 10 having a shape according to Fig. 4 arises.
- the stamped part 40 has recesses 42. These recesses 42 extend into the plane of the fins 16.
- the lower edges 28, 32 of the front longitudinal sections 22 and the rear longitudinal sections 24 of the fins 16 are rectilinear. Adjacent to these lower edges 28, 32 edge portions 36 which can be angled inwardly or outwardly relative to the plane of the longitudinal sections 22, 24. If they are angled inward, this creates a vortex generator 10, the shape of the vortex generator 10 from Fig. 5 equivalent.
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Abstract
Vortex-Generator mit einer Längsrichtung, zwei Finnen, die jeweils in einem Winkel zu der Längsrichtung angeordnet sind und sich in der Längsrichtung über eine erste Länge erstrecken, und einer Basis, die die beiden Finnen miteinander verbindet, die eine Breite aufweist und sich in der Längsrichtung über eine zweite Länge erstreckt, wobei über die gesamte Breite der Basis die zweite Länge kleiner ist als die erste Länge.A vortex generator having a longitudinal direction, two fins each disposed at an angle to the longitudinal direction and extending in the longitudinal direction over a first length, and a base connecting the two fins having a width and extending in the Extending longitudinally over a second length, wherein over the entire width of the base, the second length is smaller than the first length.
Description
Die Erfindung betrifft einen Vortex-Generator zur Befestigung an einem Windenergieanlagenrotorblatt. Vortex-Generatoren, gelegentlich auch als Wirbelerzeuger bezeichnet, werden bei Windenergieanlagenrotorblättern für eine gezielte Beeinflussung der Strömungsverhältnisse eingesetzt. Sie weisen zwei in einem Abstand voneinander angeordnete Finnen auf, die jeweils von der Oberfläche des Rotorblatts in eine Grenzschicht der Strömung hineinragen und die in einem Winkel zur Anströmrichtung ausgerichtet sind. Sind diese Finnen im Betrieb des Rotorblatts der anströmenden Luft ausgesetzt, führt dies zur Ausbildung von energiereichen Wirbeln und stromabwärts des Vortex-Generators zu einer turbulenten Grenzschicht. Insbesondere im Blattwurzelbereich hat es sich in vielen Fällen als sinnvoll herausgestellt, diesen Effekt zur Vermeidung oder Verzögerung von Strömungsablösungen einzusetzen. Hierzu müssen die Vortex-Generatoren an geeigneten Positionen auf der Blattoberfläche befestigt werden. Dies geschieht in der Regel durch Aufkleben.The invention relates to a vortex generator for attachment to a wind turbine rotor blade. Vortex generators, sometimes referred to as vortex generators, are used in wind turbine rotor blades for a specific influencing of the flow conditions. They have two fins arranged at a distance from each other, each projecting from the surface of the rotor blade into a boundary layer of the flow and which are aligned at an angle to the direction of flow. If these fins are exposed to the incoming air in the operation of the rotor blade, this leads to the formation of high-energy vortices and downstream of the vortex generator to a turbulent boundary layer. In particular, in the leaf root area, it has been found useful in many cases to use this effect to avoid or delay flow separation. For this purpose, the vortex generators must be attached to appropriate positions on the leaf surface. This is usually done by sticking.
Diese Befestigung begegnet erheblichen Schwierigkeiten. Grundsätzlich bestehen hohe Anforderungen an die Qualität der Befestigung, denn im Betrieb sind die Rotorblätter von Windenergieanlagen jahrelang Wind und Wetter ausgesetzt und für Wartungs- und Reparaturarbeiten schwer zugänglich. Hinzu kommt, dass die Oberfläche der Rotorblätter eine Krümmung aufweist, die sich sowohl in Richtung der Blatttiefe, also von der Profilnasenkante zur Profilendkante hin, als auch in Längsrichtung des Rotorblatts, also von der Blattwurzel zur Blattspitze hin, fortwährend ändert.This attachment encounters considerable difficulties. Basically, there are high demands on the quality of the attachment, because during operation, the rotor blades of wind turbines are exposed to wind and weather for years and difficult to access for maintenance and repair work. In addition, the surface of the rotor blades has a curvature that changes continuously both in the direction of the blade depth, ie from the profile nose edge to the profile end edge, and in the longitudinal direction of the rotor blade, ie from the blade root to the blade tip.
Eine individuelle Anpassung der Befestigungsfläche jedes Vortex-Generators an die an der Position seiner vorgesehenen Befestigung bestehende Krümmung der Oberfläche des Rotorblatts ist nicht praktikabel. Darum wird für die Befestigungsflächen der Vortex-Generatoren eine ebene Fläche oder eine Fläche mit einer mittleren Krümmung gewählt. Die unvermeidlichen Spalte müssen mit Klebstoff aufgefüllt werden. Hierfür ist ein relativ dünnflüssiger Klebstoff erforderlich, der eine geringe Anfangshaftung aufweist, sodass jeder Vortex-Generator fixiert werden muss, bis der Klebstoff eine ausreichende Haftung bietet. Klebebänder stellen keine geeignete Alternative dar, da sie zum Ausgleich unterschiedlicher Spaltmaße nur sehr bedingt geeignet sind. Die Montage der Vortex-Generatoren ist daher aufwendig und fehleranfällig. In der Praxis ist immer wieder zu beobachten, dass sich einzelne Vortex-Generatoren von der Oberfläche lösen und schließlich abfallen.An individual adaptation of the mounting surface of each vortex generator to the curvature of the surface of the rotor blade existing at the position of its intended attachment is impractical. Therefore, a plane surface or an area with a mean curvature is selected for the attachment surfaces of the vortex generators. The inevitable gaps must be filled up with glue become. This requires a relatively low viscosity adhesive that has low initial tack, so any vortex generator needs to be fixed until the adhesive provides adequate adhesion. Adhesive tapes do not represent a suitable alternative since they are only of limited suitability to compensate for different gap dimensions. The assembly of the vortex generators is therefore complicated and error-prone. In practice it can be observed again and again that individual vortex generators detach from the surface and eventually fall off.
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Davon ausgehend ist es die Aufgabe der Erfindung, einen Vortex-Generator zur Verfügung zu stellen, der besonders einfach und zuverlässig an einer Oberfläche eines Windenergieanlagenrotorblatts befestigt werden kann.On this basis, it is the object of the invention to provide a vortex generator which can be attached to a surface of a wind turbine rotor blade in a particularly simple and reliable manner.
Diese Aufgabe wird gelöst durch den Vortex-Generator mit den Merkmalen des Anspruchs 1. Vorteilhafte Ausgestaltungen sind in den Unteransprüchen angegeben.This object is achieved by the vortex generator having the features of claim 1. Advantageous embodiments are specified in the subclaims.
Der Vortex-Generator hat eine Längsrichtung, zwei Finnen, die jeweils in einem Winkel zu der Längsrichtung angeordnet sind und sich in der Längsrichtung über eine erste Länge erstrecken, und eine Basis, die die beiden Finnen miteinander verbindet, wobei die Basis eine Breite aufweist und sich in der Längsrichtung über eine zweite Länge erstreckt, wobei über die gesamte Breite der Basis die zweite Länge kleiner ist als die erste Länge.The vortex generator has a longitudinal direction, two fins each arranged at an angle to the longitudinal direction and extending in the longitudinal direction over a first length, and a base connecting the two fins with each other, wherein the base has a width and extending in the longitudinal direction over a second length, wherein over the entire width of the base, the second length is smaller than the first length.
Die Längsrichtung entspricht einer Auslegungsanströmrichtung, also derjenigen Richtung, in der der Vortex-Generator im regulären Betrieb von der anströmenden Luft angeströmt wird. Ist der Vortex-Generator an der Oberfläche eines Windenergieanlagenrotorblatts befestigt, liegt die Längsrichtung in einer Profilebene des Rotorblatts. Die zu einer Profilnasenkante des Rotorblatts weisende Richtung wird als vorn, die zu einer Profilendkante weisende Richtung wird als hinten bezeichnet. In ähnlicher Weise bezieht sich die Angabe unten auf die zu der Oberfläche des Rotorblatts weisende Richtung und die Angabe oben auf die sich von dieser Oberfläche entfernende Richtung.The longitudinal direction corresponds to a Auslegungsanströmrichtung, ie the direction in which the vortex generator is flowed in the regular operation of the incoming air. If the vortex generator is attached to the surface of a wind turbine rotor blade, the longitudinal direction lies in a profile plane of the rotor blade. The direction pointing to a profile nose edge of the rotor blade is called forward, the direction pointing to a profile end edge is referred to as the rear. Similarly, the indication below refers to the direction toward the surface of the rotor blade and the indication above refers to the direction away from that surface.
Die Finnen erstrecken sich ausgehend von der Basis nach oben, insbesondere etwa orthogonal zur Oberfläche des Windenergieanlagenrotorblatts. Sie können jedoch auch davon abweichend mehr oder weniger stark geneigt zu der Oberfläche angeordnet sein. Die Finnen weisen eine Höhe auf, die an die Dicke einer Grenzschicht der Strömung angepasst sein kann. Insbesondere kann die Höhe etwas größer sein als die Dicke der Grenzschicht. Die Finnen können über ihre gesamte Länge eine gleichmäßige Höhe aufweisen. Alternativ kann die Höhe über die Längsrichtung variieren. Gebräuchlich sind insbesondere Vortex-Generatoren, deren Höhe an einem vorderen Ende geringer ist als einem hinteren Ende. In diesem Fall können die Finnen im Wesentlichen trapezförmig bzw. dreieckig ausgebildet sein. Abweichungen davon sind möglich, sowohl mit gekrümmt verlaufenden Vorder-, Hinter-, Ober- und/oder Unterkanten, als auch mit mehr oder weniger stark abgerundeten Ecken.The fins extend upwardly from the base, in particular approximately orthogonally to the surface of the wind turbine rotor blade. However, you can also deviating more or less inclined to the surface arranged be. The fins have a height that can be adapted to the thickness of a boundary layer of the flow. In particular, the height may be slightly larger than the thickness of the boundary layer. The fins may have a uniform height over their entire length. Alternatively, the height may vary over the lengthwise direction. In particular, vortex generators whose height is less at a front end than a rear end are common. In this case, the fins may be substantially trapezoidal or triangular. Deviations are possible, both with curved front, rear, upper and / or lower edges, as well as with more or less rounded corners.
Eine Fläche, in der die betreffende Finne angeordnet ist, kann eben oder leicht gekrümmt sein. Beide Finnen sind in einem Winkel zu der Längsrichtung angeordnet. Dieser Winkel kann beispielsweise im Bereich von 5° bis 45° liegen, sodass die beiden Finnen relativ zueinander in einem Winkel im Bereich von 10° bis 90° ausgerichtet sind. Die beiden Finnen können insbesondere spiegelsymmetrisch zu einer in der Längsrichtung ausgerichteten Längsachse des Vortex-Generators angeordnet sein.A surface in which the respective fin is arranged may be flat or slightly curved. Both fins are arranged at an angle to the longitudinal direction. This angle may be, for example, in the range of 5 ° to 45 °, so that the two fins are oriented relative to each other at an angle in the range of 10 ° to 90 °. The two fins can in particular be arranged mirror-symmetrically to a longitudinal axis of the vortex generator aligned in the longitudinal direction.
Eine Besonderheit der Erfindung besteht darin, dass über die gesamte Breite der Basis die zweite Länge kleiner ist als die erste Länge, dass sich mit anderen Worten die Basis also in Strömungsrichtung nicht über die gesamte Länge der Finnen erstreckt. Mit der Erstreckung der Basis in der Längsrichtung ist die gesamte Ausdehnung der Basis in dieser Richtung gemeint, also von einem in Strömungsrichtung am weitesten vorn befindlichen Punkt der Basis bis zu einem am weitesten hinten befindlichen Punkt der Basis. Beispielsweise kann die Basis streifenförmig ausgebildet sein mit parallel angeordneten Vorder- und Hinterkanten. In diesem Fall entspricht der Abstand zwischen der Vorderkante und der Hinterkante der Basis der zweiten Länge. Quer zu der Längsrichtung weist die Basis eine Breite auf, die sich von der einen Finne bis zu der anderen Finne erstreckt. Wegen der Winkelstellung der Finnen kann die Basis bei auf die Oberfläche gerichteter Blickrichtung insbesondere trapezförmig ausgebildet sein. Alternativ kann die Basis auch seitlich über die Finnen überstehen.A special feature of the invention is that over the entire width of the base, the second length is smaller than the first length, that in other words the base does not extend in the flow direction over the entire length of the fins. By the extension of the base in the longitudinal direction is meant the entire extent of the base in this direction, that is, from a forwardmost point of the base to a rearmost point of the base. For example, the base may be strip-shaped with parallel front and rear edges. In this case, the distance between the leading edge and the trailing edge of the base corresponds to the second length. Transverse to the longitudinal direction, the base has a width extending from one fin to the other fin. Because of the angular position of the fins For example, the base may be trapezoidal in particular when the viewing direction is directed towards the surface. Alternatively, the base can also survive laterally over the fins.
Typische Abmessungen des gesamten Vortex-Generators liegen beispielsweise in einem Bereich zwischen einer Länge von 2 cm und einer Breite von 1,5 cm bis zu einer Länge von 25 cm und einer Breite von 20 cm, wobei die Höhe der Finnen beispielsweise in einem Bereich zwischen 20 % und 100 % der Länge liegen kann. Die Basis oder der gesamte Vortex-Generator kann aus einem relativ steifen, unflexiblen Material wie beispielsweise Metall bestehen. Ein Faserverbundmaterial stellt eine Alternative dar. Der Vortex-Generator kann einteilig gefertigt oder aus mehreren Elementen zusammengesetzt sein.Typical dimensions of the entire vortex generator are, for example, in a range between a length of 2 cm and a width of 1.5 cm to a length of 25 cm and a width of 20 cm, the height of the fins, for example, in a range between 20% and 100% of the length can be. The base or the entire vortex generator may consist of a relatively stiff, inflexible material such as metal. A fiber composite material is an alternative. The vortex generator can be made in one piece or composed of several elements.
Die Erfindung macht sich zunutze, dass bei Windenergieanlagenrotorblättern die positionsabhängige Änderung der Krümmung der Oberfläche in der Längsrichtung besonders ausgeprägt ist. Durch das vorgesehene Verkürzen der Länge der Basis in dieser Längsrichtung verringern sich die zwischen der Befestigungsfläche und der Oberfläche des Rotorblatts auftretenden Spaltmaße. Die Erfinder haben erkannt, dass die auftretenden Spaltmaße bei einer hinreichend kurzen Basis so weit verkleinert werden können, dass sie zum Beispiel durch die Elastizität eines doppelseitigen Klebebands ausgeglichen werden können. Beispielsweise können Klebebänder mit einer Stärke von 1,5 mm eingesetzt werden, die aufgrund ihrer Elastizität einen Ausgleich bis zu etwa 25 % ihrer Dicke herbeiführen können. Wird die Basis soweit verkürzt, dass sich die Größe der an den unterschiedlichen Befestigungspositionen auftretenden Spalte um nicht mehr als etwa 0,375 mm ändert, ist demnach eine zuverlässige und besonders einfache Befestigung mit einem solchen Klebeband möglich. Vorteile ergeben sich jedoch auch bei Verwendung anderer Klebstoffe.The invention makes use of the fact that in the case of wind turbine rotor blades the position-dependent change of the curvature of the surface in the longitudinal direction is particularly pronounced. The intended shortening of the length of the base in this longitudinal direction reduces the gaps which occur between the fastening surface and the surface of the rotor blade. The inventors have recognized that the gap dimensions that occur can be reduced to a sufficiently short base so that they can be compensated, for example, by the elasticity of a double-sided adhesive tape. For example, 1.5 mm thick tapes can be used, which due to their elasticity, can compensate for up to about 25% of their thickness. If the base is shortened so much that the size of the gaps occurring at the different attachment positions does not change by more than about 0.375 mm, then a reliable and particularly simple attachment with such an adhesive tape is possible. However, advantages also arise when using other adhesives.
In einer Ausgestaltung beträgt die zweite Länge höchstens 70 % der ersten Länge. Die zweite Länge kann auch höchstens 50 %, höchstens 40 %, höchstens 30 % oder höchstens 20 % der ersten Länge betragen. Durch diese Maßnahme ist eine weitere Verringerung der auftretenden Spaltmaße möglich, sodass eine zuverlässige Befestigung auch bei großen Vortex-Generatoren gelingt. Versuche haben gezeigt, dass die Größe der verbleibenden Befestigungsfläche trotz der Verkürzung in vielen Fällen ausreichend ist.In one embodiment, the second length is at most 70% of the first length. The second length may also be at most 50%, at most 40%, at most 30% or not more than 20% of the first length. By this measure, a further reduction of the gap dimensions occurring is possible, so that a reliable attachment succeeds even with large vortex generators. Experiments have shown that the size of the remaining attachment surface in spite of the shortening is sufficient in many cases.
In einer Ausgestaltung weist die Basis eine Befestigungsfläche zur Verklebung mit einer Oberfläche eines Windenergieanlagenrotorblatts auf. Die Befestigungsfläche befindet sich an einer Unterseite der Basis. Die Befestigungsfläche kann sich wahlweise über die gesamte Unterseite der Basis erstrecken oder über einen Teil davon, insbesondere über einen Großteil der Gesamtfläche der Unterseite der Basis. Außerdem kann die Befestigungsfläche eine aktivierte Oberfläche aufweisen, um eine besonders sichere Verbindung mit dem Klebstoff zu gewährleisten.In one embodiment, the base has a mounting surface for bonding to a surface of a wind turbine rotor blade. The attachment surface is located at an underside of the base. The attachment surface may optionally extend over the entire underside of the base or over a portion thereof, in particular over much of the total area of the underside of the base. In addition, the mounting surface may have an activated surface to ensure a particularly secure connection with the adhesive.
In einer Ausgestaltung weist die Befestigungsfläche in der Längsrichtung eine Krümmung auf. Grundsätzlich kann die Befestigungsfläche auch eben sein. Eine insbesondere konkave Krümmung erlaubt jedoch eine weitere Verringerung der auftretenden Spaltmaße, insbesondere wenn sie an eine mittlere Krümmung der Oberfläche des Windenergieanlagenrotorblatts angepasst ist.In one embodiment, the attachment surface has a curvature in the longitudinal direction. In principle, the mounting surface can also be flat. However, a particularly concave curvature allows a further reduction in the gap dimensions that occur, in particular if it is adapted to a mean curvature of the surface of the wind turbine rotor blade.
In einer Ausgestaltung weisen die Finnen jeweils einen mittleren Längsabschnitt auf, dessen untere Kante mit der Basis verbunden ist, sowie einen vorderen Längsabschnitt, der in der Längsrichtung vor der Basis angeordnet ist, und ein hinteren Längsabschnitt, der in der Längsrichtung hinter der Basis angeordnet ist. In diesem Fall sind der vordere Längsabschnitt und der hintere Längsabschnitt nicht unmittelbar mit der Basis verbunden. Die Basis befindet sich jedoch in einer mittleren Position und die Finnen sind über ihre gesamte Länge hinreichend fixiert. Eine Befestigung des vorderen Längsabschnitts oder des hinteren Längsabschnitts an der Oberfläche des Rotorblatts ist bei der Erfindung nicht erforderlich und auch nicht vorgesehen. Davon unabhängig kann eine Versiegelung des Freiraums zwischen den genannten Längsabschnitten und der Oberfläche des Rotorblatts sinnvoll sein.In one embodiment, the fins each have a central longitudinal portion, the lower edge of which is connected to the base, and a front longitudinal portion, which is arranged in front of the base in the longitudinal direction, and a rear longitudinal portion, which is arranged in the longitudinal direction behind the base , In this case, the front longitudinal portion and the rear longitudinal portion are not connected directly to the base. However, the base is in a middle position and the fins are sufficiently fixed over their entire length. An attachment of the front longitudinal section or the rear longitudinal section on the surface of the rotor blade is not required in the invention and also not provided. Regardless of this, a sealing of the free space between the longitudinal sections mentioned and the surface of the rotor blade can be useful.
In einer Ausgestaltung ist der vordere Längsabschnitt in einer Ebene angeordnet und weist eine untere Kante auf, die nach unten über die Basis übersteht und/oder der hintere Längsabschnitt ist in einer Ebene angeordnet und weist eine untere Kante auf, die nach unten über die Basis übersteht. Insbesondere bei stark gekrümmten Oberflächen kann auf diese Weise der Abstand zwischen den unteren Kanten der Finnen und der Oberfläche des Rotorblatts verringert werden, was aerodynamisch vorteilhaft sein kann.In one embodiment, the front longitudinal portion is arranged in a plane and has a lower edge projecting down over the base and / or the rear longitudinal portion is arranged in a plane and has a lower edge which projects down over the base , In particular, in the case of strongly curved surfaces, the distance between the lower edges of the fins and the surface of the rotor blade can be reduced in this way, which can be aerodynamically advantageous.
In einer Ausgestaltung ist die untere Kante des vorderen Längsabschnitts und/oder die untere Kante des hinteren Längsabschnitts gekrümmt. Insbesondere können diese Kanten an eine mittlere Krümmung oder an eine minimale Krümmung der Oberfläche des Windenergieanlagenrotorblatts angepasst sein. Die Krümmung kann zu einem geringen Abstand zwischen Finne und Oberfläche beitragen.In one embodiment, the lower edge of the front longitudinal section and / or the lower edge of the rear longitudinal section is curved. In particular, these edges may be adapted to a mean curvature or to a minimum curvature of the surface of the wind turbine rotor blade. The curvature can contribute to a small distance between the fin and the surface.
In einer Ausgestaltung weist ein vorderer Längsabschnitt und/oder ein hinterer Längsabschnitt einer Finne an seiner unteren Kante einen abgewinkelten Randabschnitt auf. Der Randabschnitt kann aus einer Ebene, in der der Längsabschnitt angeordnet ist, herausstehen. Insbesondere kann er sich von der Kante nach außen, also von der anderen Finne weg, oder nach innen, als zu der anderen Finne hin, erstrecken. Der abgewinkelte Randabschnitt bewirkt eine Versteifung der Finne und kann Vibrationen entgegenwirken.In one embodiment, a front longitudinal section and / or a rear longitudinal section of a fin has an angled edge section at its lower edge. The edge portion may protrude from a plane in which the longitudinal portion is arranged. In particular, it may extend from the edge to the outside, that is, away from the other fin, or to the inside, than toward the other fin. The angled edge section causes a stiffening of the fin and can counteract vibrations.
In einer Ausgestaltung ist der Vortex-Generator durch Ausstanzen eines Flachmaterials und anschließendes Abwinkeln der beiden Finnen relativ zu der Basis hergestellt. Diese Art der Fertigung ist besonders einfach. Durch das Abwinkeln wird eine hohe Formstabilität erreicht. Das Flachmaterial kann insbesondere ein Blech sein, beispielsweise aus Aluminium oder Stahl, insbesondere Edelstahl. Das Flachmaterial kann eine gleichmäßige Dicke aufweisen, beispielsweise im Bereich von 0,3 mm bis 3 mm. Wahlweise können die bereits erwähnten Randabschnitte an den unteren Kanten vorderer und/oder hinterer Längsabschnitte der Finnen ebenfalls durch einfaches Abwinkeln geformt werden.In one embodiment, the vortex generator is manufactured by punching out a flat material and then bending the two fins relative to the base. This type of production is particularly easy. By bending a high dimensional stability is achieved. The flat material may in particular be a sheet, for example made of aluminum or steel, in particular stainless steel. The flat material may have a uniform thickness, for example in the range of 0.3 mm to 3 mm. Optionally, the aforementioned edge portions at the lower edges of front and / or rear longitudinal portions of the fins can also be formed by simple angling.
In einer Ausgestaltung ist ein doppelseitiges Klebeband auf die Befestigungsfläche aufgeklebt. Das Klebeband kann eine elastische Schicht aufweisen, insbesondere aus Schaumstoff und/oder mit einer Dicke von beispielsweise 1 mm oder mehr. Dies ermöglicht den bereits erläuterten Ausgleich von unterschiedlichen Spaltmaßen. Der Vortex-Generator kann ohne weitere Vorarbeiten besonders einfach auf die Oberfläche eines Windenergieanlagenrotorblatts aufgeklebt werden.In one embodiment, a double-sided adhesive tape is adhered to the mounting surface. The adhesive tape may have an elastic layer, in particular made of foam and / or with a thickness of, for example, 1 mm or more. This allows the already explained compensation of different gaps. The vortex generator can be particularly easily glued to the surface of a wind turbine rotor blade without further preparation.
In einer Ausgestaltung erstreckt sich das doppelseitige Klebeband über die gesamte Breite der Befestigungsfläche bzw. der Basis und/oder über die gesamte zweite Länge. Dies ermöglicht eine vollflächige Verklebung.In one embodiment, the double-sided adhesive tape extends over the entire width of the attachment surface or the base and / or over the entire second length. This allows a full-surface bonding.
In einer Ausgestaltung ist ein Vortex-Generator nach einem der Ansprüche 1 bis 11 mit einem Windenergieanlagenrotorblatt kombiniert, wobei die Befestigungsfläche des Vortex-Generators mit einer Oberfläche des Windenergieanlagenrotorblatts verklebt ist. Die Verklebung kann insbesondere mit einem doppelseitigen Klebeband hergestellt sein.In one embodiment, a vortex generator according to any one of claims 1 to 11 is combined with a wind turbine rotor blade, wherein the mounting surface of the vortex generator is bonded to a surface of the wind turbine rotor blade. The bond can be made in particular with a double-sided adhesive tape.
In einer Ausgestaltung ist zwischen der Oberfläche und an die Oberfläche angrenzenden Kanten des Vortex-Generators eine Versiegelung angeordnet. Die Versiegelung kann beispielsweise mit einer Dichtmasse, etwa einem Silikonwerkstoff, ausgeführt sein. Sie kann um die Befestigungsfläche umlaufen und/oder zwischen unteren Kanten der Finnen und der Oberfläche angeordnet sein. Durch die Versiegelung wird einerseits die Verklebung vor äußeren Einflüssen geschützt. Andererseits kann einer Ansammlung von Verschmutzungen vorgebeugt werden. Weiterhin führt die Versiegelung zu einer optimalen aerodynamischen Form.In one embodiment, a seal is disposed between the surface and edges of the vortex generator adjacent the surface. The seal can be performed, for example, with a sealant, such as a silicone material. It may orbit around the attachment surface and / or be disposed between lower edges of the fins and the surface. On the one hand, the seal protects the bond from external influences. On the other hand, accumulation of soiling can be prevented. Furthermore, the seal leads to an optimal aerodynamic shape.
In einer Ausgestaltung sind mehrere, identisch geformte Vortex-Generatoren an verschiedenen Positionen der Oberfläche, an denen die Oberfläche unterschiedliche Krümmungen aufweist, mit der Oberfläche verklebt. Eine individuelle Anpassung der Geometrie der Vortex-Generatoren an unterschiedlich stark gekrümmte Oberflächen ist bei der Erfindung nicht notwendig.In one embodiment, a plurality of identically shaped vortex generators are bonded to the surface at different positions on the surface where the surface has different curvatures. An individual adaptation of the geometry of the vortex generators to differently curved surfaces is not necessary in the invention.
Nachfolgend wird die Erfindung anhand von in Figuren dargestellten Ausführungsbeispielen näher erläutert. Es zeigen:
- Figur 1
- ein Windenergieanlagenrotorblatt mit Vortex-Generatoren
- Figuren 2-6
- jeweils ein Ausführungsbeispiel eines Vortex-Generators, im linken Teil der Figur in einer Ansicht von der Seite und im rechten Teil der Figur in einer Ansicht von oben;
- Figuren 7 und 8
- jeweils ein Stanzteil zur Herstellung eines Vortex-Generators in einer Draufsicht.
- FIG. 1
- a wind turbine rotor blade with vortex generators
- Figures 2-6
- in each case an embodiment of a vortex generator, in the left part of the figure in a view from the side and in the right part of the figure in a view from above;
- FIGS. 7 and 8
- in each case a stamped part for producing a vortex generator in a plan view.
Alle Figuren sind schematisch. Ein Pfeil kennzeichnet in jeder Figur die der Auslegungsanströmrichtung entsprechende Längsrichtung 12.All figures are schematic. An arrow in each figure indicates the
Der Vortex-Generator 10 aus
Die Basis 18 ist streifenförmig ausgebildet, wobei sich die Breite B des Streifens quer zur Längsrichtung 12 erstreckt. In der im rechten Teil der
Die Finnen 16 weisen eine Höhe H auf, die an ihrem hinteren Ende größer ist als an ihrem vorderen Ende. Vor dem mittleren Längsabschnitt 20 ist ein vorderer Längsabschnitt 22 angeordnet, der nicht unmittelbar mit der Basis 18 verbunden ist. Hinter dem mittleren Längsabschnitt 20 ist ein hinterer Längsabschnitt 24 angeordnet, der ebenfalls nicht unmittelbar mit der Basis 18 verbunden ist. Die drei Längsabschnitte 20, 22, 24 der Finnen 16 sind jeweils in einer Ebene angeordnet, die senkrecht zur Basis bzw. zu Oberfläche 14 des Windenergieanlagenrotorblatts ausgerichtet ist und in einem Winkel α zur Längsrichtung 12.The
Im rechten Teil der
Der vordere Längsabschnitt 22 weist eine untere Kante 28 auf. Der mittlere Längsabschnitt 20 weist eine untere Kante 30 auf, an der die Finne 16 in die Basis 18 übergeht. Der hintere Längsabschnitt 24 weist eine untere Kante 32 auf. Die unteren Kanten 28, 30, 32 sind im Ausführungsbeispiel der
Der Vortex-Generator 10 aus
Der Vortex-Generator 10 aus
Der Vortex-Generator 10 aus
Der Vortex-Generator 10 aus
Bei dem Stanzteil 40 aus
- 1010
- Vortex-GeneratorVortex generator
- 1212
- Längsrichtunglongitudinal direction
- 1414
- Oberflächesurface
- 1616
- Finnefin
- 1818
- BasisBase
- 2020
- mittlerer Längsabschnittmiddle longitudinal section
- 2222
- vorderer Längsabschnittfront longitudinal section
- 2424
- hinterer Längsabschnittrear longitudinal section
- 2626
- Längsachselongitudinal axis
- 2828
-
untere Kante des vorderen Längsabschnitts 22lower edge of the front
longitudinal section 22 - 3030
-
untere Kante des mittleren Längsabschnitts 20lower edge of the central
longitudinal section 20 - 3232
-
untere Kante des hinteren Längsabschnitts 24lower edge of the rear
longitudinal section 24 - 3434
- doppelseitiges Klebebanddouble-sided adhesive tape
- 3636
- Randabschnittedge section
- 3838
- Versiegelungsealing
- 4040
- Stanzteilstamping
- 4242
- Aussparungrecess
- 100100
- WindenergieanlagenrotorblattWind turbine rotor blade
- 106106
- RotorblattwurzelbereichRotor blade root area
- 107107
- ÜbergangsbereichTransition area
- 108108
- ProfilbereichFocus area
- 109109
- Druckseitepressure side
- 110110
- Saugseitesuction
- 111111
- LängserstreckungsrichtungLongitudinal extension
- L1L1
- erste Längefirst length
- L2L2
- zweite Längesecond length
- BB
- Breitewidth
Claims (15)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK18161546.9T DK3540211T3 (en) | 2018-03-13 | 2018-03-13 | Vortex generator for attachment to a wind turbine blade |
EP18161546.9A EP3540211B1 (en) | 2018-03-13 | 2018-03-13 | Vortex generator for attachment to a wind energy assembly rotor blade |
US16/352,637 US11174834B2 (en) | 2018-03-13 | 2019-03-13 | Vortex generator for fastening to a wind turbine rotor blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP18161546.9A EP3540211B1 (en) | 2018-03-13 | 2018-03-13 | Vortex generator for attachment to a wind energy assembly rotor blade |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3540211A1 true EP3540211A1 (en) | 2019-09-18 |
EP3540211B1 EP3540211B1 (en) | 2021-11-10 |
Family
ID=61628246
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18161546.9A Active EP3540211B1 (en) | 2018-03-13 | 2018-03-13 | Vortex generator for attachment to a wind energy assembly rotor blade |
Country Status (3)
Country | Link |
---|---|
US (1) | US11174834B2 (en) |
EP (1) | EP3540211B1 (en) |
DK (1) | DK3540211T3 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3690230B1 (en) | 2019-01-30 | 2022-11-16 | Nordex Energy SE & Co. KG | Vortex generator with a single fin |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6783212B2 (en) * | 2017-10-20 | 2020-11-11 | 三菱重工業株式会社 | How to position the vortex generator on the wind turbine wing, how to manufacture the wind turbine wing assembly and the wind turbine wing assembly |
DE102018121190A1 (en) * | 2018-08-30 | 2020-03-05 | Wobben Properties Gmbh | Rotor blade, wind turbine and method for optimizing a wind turbine |
US20220325688A1 (en) * | 2018-09-11 | 2022-10-13 | Littoral Power Systems, Inc. | Hydrokinetic energy device |
EP4321749A1 (en) * | 2022-08-12 | 2024-02-14 | Wobben Properties GmbH | Wind power plant and vortex generator therefor |
Citations (7)
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US20120151769A1 (en) * | 2010-12-16 | 2012-06-21 | Inventus Holdings, Llc | Method for determining optimum vortex generator placement for maximum efficiency on a retrofitted wind turbine generator of unknown aerodynamic design |
EP2484898A1 (en) | 2011-02-04 | 2012-08-08 | LM Wind Power A/S | Vortex generator device with tapered sections for a wind turbine |
WO2013014082A2 (en) * | 2011-07-22 | 2013-01-31 | Lm Wind Power A/S | Wind turbine blade comprising vortex generators |
EP2799709A1 (en) | 2013-05-02 | 2014-11-05 | General Electric Company | Attachment system and method for wind turbine vortex generators |
EP2826708A2 (en) | 2013-05-03 | 2015-01-21 | General Electric Company | Wind turbine rotor blade assembly with surface features |
WO2015030573A1 (en) | 2013-09-02 | 2015-03-05 | Corten Holding Bv | Vortex generator for a wind turbine |
CN207420779U (en) * | 2017-10-26 | 2018-05-29 | 上海绿孚科技有限公司 | A kind of new blade of wind-driven generator vortex generator for being beneficial to installation |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2627790T3 (en) * | 2005-05-17 | 2017-07-31 | Vestas Wind Systems A/S | Pitch controlled wind turbine blade that has turbulence generation means, wind turbine and use of it |
US11015569B2 (en) * | 2015-11-12 | 2021-05-25 | Mitsubishi Heavy Industries, Ltd. | Vortex generator, wind turbine blade, and wind turbine power generating apparatus |
US20180038342A1 (en) * | 2016-08-05 | 2018-02-08 | General Electric Company | Vortex generators for wind turbine rotor blades |
-
2018
- 2018-03-13 EP EP18161546.9A patent/EP3540211B1/en active Active
- 2018-03-13 DK DK18161546.9T patent/DK3540211T3/en active
-
2019
- 2019-03-13 US US16/352,637 patent/US11174834B2/en active Active
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120151769A1 (en) * | 2010-12-16 | 2012-06-21 | Inventus Holdings, Llc | Method for determining optimum vortex generator placement for maximum efficiency on a retrofitted wind turbine generator of unknown aerodynamic design |
EP2484898A1 (en) | 2011-02-04 | 2012-08-08 | LM Wind Power A/S | Vortex generator device with tapered sections for a wind turbine |
WO2013014082A2 (en) * | 2011-07-22 | 2013-01-31 | Lm Wind Power A/S | Wind turbine blade comprising vortex generators |
EP2799709A1 (en) | 2013-05-02 | 2014-11-05 | General Electric Company | Attachment system and method for wind turbine vortex generators |
EP2826708A2 (en) | 2013-05-03 | 2015-01-21 | General Electric Company | Wind turbine rotor blade assembly with surface features |
WO2015030573A1 (en) | 2013-09-02 | 2015-03-05 | Corten Holding Bv | Vortex generator for a wind turbine |
CN207420779U (en) * | 2017-10-26 | 2018-05-29 | 上海绿孚科技有限公司 | A kind of new blade of wind-driven generator vortex generator for being beneficial to installation |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3690230B1 (en) | 2019-01-30 | 2022-11-16 | Nordex Energy SE & Co. KG | Vortex generator with a single fin |
Also Published As
Publication number | Publication date |
---|---|
EP3540211B1 (en) | 2021-11-10 |
US20190285046A1 (en) | 2019-09-19 |
US11174834B2 (en) | 2021-11-16 |
DK3540211T3 (en) | 2022-02-14 |
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